## 48429 Federal Register / Vol. 77, No. 157 / Tuesday, August 14, 2012 / Rules and Regulations

(e) Reason

This AD was prompted by a report of a capacitive density condensator (cadensicon) coil overheating during testing. We are issuing this AD to detect and correct potential overheating of the cadensicon coil, which could create an ignition source inside a fuel tank, which, in combination with flammable fuel vapors, could result in a fuel tank explosion and consequent loss of the airplane.
(f) Compliance

You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.
(g) Actions

Within 30 months after the effective date of this AD, inspect to determine whether any fuel quantity indication computer (FQIC) Type 1, having part number (P/N) SIC5054 or P/N SIC5051 (as applicable to the airplane model), is installed, in accordance with the Accomplishment Instructions of Airbus Mandatory Service Bulletin A300–28–6024, Revision 02, dated January 19, 2011; or Airbus Mandatory Service Bulletin A310–28– 2039, Revision 01, dated January 19, 2011; as applicable. A review of airplane maintenance records is acceptable in lieu of this inspection if the part number of the FQIC can be conclusively determined from that review. If any FQIC Type 1 having P/N SIC5054 or P/N SIC5051 is installed, within 30 months after the effective date of this AD, replace the FQIC Type 1 with a FQIC Type 2 having P/ N SIC5055, P/N SIC5076, P/N SIC5082, or P/ N SIC5083 (as applicable to Model A310 series airplanes) or with a FQIC Type 2 having P/N SIC5077 (as applicable to Model A300 B4–600 series airplanes), and modify the associated wiring, in accordance with the Accomplishment Instructions of Airbus Mandatory Service Bulletin A300–28–6024, Revision 02, dated January 19, 2011; or Airbus Mandatory Service Bulletin A310–28– 2039, Revision 01, dated January 19, 2011; as applicable.
(h) Parts Installation Prohibition

As of the effective date of this AD, no person may install any FQIC Type 1 having P/N SIC5054 or P/N SIC5051, on any airplane.
(i) Other FAA AD Provisions

The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM–116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Branch, send it to Attn: Dan Rodina, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, Washington 98057– 3356; telephone (425) 227–2125; fax (425) 227–1149. Information may be emailed to: 9– ANM–116–AMOC–REQUESTS@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/ certificate holding district office. The AMOC approval letter must specifically reference this AD.

(2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service.
(j) Related Information

Refer to MCAI European Aviation Safety Agency Airworthiness Directive 2011–0186, dated September 23, 2011, and the service information specified in paragraphs (j)(1) and (j)(2) of this AD, for related information.

(1) Airbus Mandatory Service Bulletin A300–28–6024, Revision 02, dated January 19, 2011.

(2) Airbus Mandatory Service Bulletin A310–28–2039, Revision 01, dated January 19, 2011. (k) Material Incorporated by Reference

(1) The Director of the Federal Register approved the incorporation by reference (IBR) of the following service information under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use the following service information to do the actions required by this AD, unless the AD specifies otherwise.

(i) Airbus Mandatory Service Bulletin A300–28–6024, Revision 02, dated January 19, 2011.

(ii) Airbus Mandatory Service Bulletin A310–28–2039, Revision 01, dated January 19, 2011.

(3) For Airbus service information identified in this AD, contact Airbus SAS— EAW (Airworthiness Office), 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email account.airwortheas@airbus.com; Internet http:// www.airbus.com.

(4) You may review copies of the service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, Washington. For information on the availability of this material at the FAA, call
425–227–1221.

(5) You may also review copies of the service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at an NARA facility, call 202–741– 6030, or go to http://www.archives.gov/ federal

_register/code

_ of

_ federal

_regulations/ ibr

_ locations.html. Issued in Renton, Washington, on July 31,
2012. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2012–19254 Filed 8–13–12; 8:45 am]

**BILLING CODE 4910–13–P** 

### DEPARTMENT OF COMMERCE

**Bureau of Industry and Security**

**15 CFR Part 774**

**The Commerce Control List**

CFR Correction

In the Federal Register published on July 26, 2012, on page 43711, in the third column, in instruction 3.C., ‘‘5A003’’ is corrected to read ‘‘5A002’’. [FR Doc. 2012–19955 Filed 8–13–12; 8:45 am]

**BILLING CODE 1505–01–D**



### FEDERAL MINE SAFETY AND HEALTH **REVIEW COMMISSION**

**29 CFR Parts 2700, 2701, 2702, 2704, 2705, 2706** 

**Commission Address Change**

**AGENCY** 

### : Federal Mine Safety and Health Review Commission (FMSHRC).

**ACTION** 

### : Final rule.

**SUMMARY** 

### : The Federal Mine Safety and Health Review Commission is relocating its Headquarters office and is amending its regulations to inform the public of the address change.

**DATES** 

### : This final rule will take effect on August 27, 2012.

**ADDRESSES** 

### : This final rule is available on FMSHRC’s Web site, http:// www.fmshrc.gov.

**FOR FURTHER INFORMATION CONTACT** 

### : Sarah Stewart, Deputy General Counsel, Office of the General Counsel, Federal Mine Safety and Health Review Commission, at (202) 434–9935 or sstewart@fmshrc.gov.

**SUPPLEMENTARY INFORMATION** 

### : A. Background

On August 24, 2012, FMSHRC will move its Headquarters office from 601 New Jersey Avenue NW., Suite 9500, Washington, DC 20001 to 1331 Pennsylvania Avenue NW., Suite 520N, Washington, DC 20004–1710.

B. Notice and Public Procedure

Because this amendment deals with agency management and procedures, the notice and comment provisions of the Administrative Procedure Act do not apply pursuant to 5 U.S.C. 553(a)(2) and (b)(3)(A).

Good cause exists to dispense with the usual 30-day delay in the effective date because the amendments are of a minor and administrative nature dealing with only a change in address.

The Commission is an independent regulatory agency and, as such, is not